N503AZ
Service difficulty reports · 32
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N503AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N503AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA20260622053Terminal · faultedDURING PRE-FLIGHT CREW REPORTED RIGHT CHART LIGHT SHOCKED PILOT WHEN TOUCHED. REMOVED AND REPLACED RIGHT CHART LIGHT IN ACCORDANCE WITH B767 AMM 33-14-00. OPERATIONAL CHECK GOOD.SDR IXXA20260609002Web · crackedNUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL SUPPORT WEB IS CRACKED REFERENCE AMES WO N503AZ-28 NR 193266-0400-0075SDR IXXA20260609001Channel · crackedNUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL O/B WEB STIFFENER IS CRACKED IN LOWER RADIUS REFERENCE AMES WO N503AZ-28 NR 193266-0400-0076SDR IXXA20260606001Strut · crackedLEFT WING L/E UPPER SUPPORT STRUCTURE HAS CRACKAT LOCK FASTENER AFT END, VERIFIED BY EDDY CURRENT AROUND LES 506SDR IXXA20260603001Rib · crackedLEFT WING L/E INTERNAL LOWER SUPPORT STRUCTURE HAS CRACK, VERFIED BY EDDY CURRENT, JUST OUTBOARD OF FUEL PANEL, REFERENCE AMES WO N503AZ-28 NR 193266-0500-0024SDR IXXA20260615CC01Skin · delaminatedDURING OK TO INSTALL LT INBD ELEVATOR FOUND INBD CORNER EDGE TO BE DAMAGED.SDR IXXA20260611CC01Structure · crackedDURING LFEC OF RH SIDE OF 1809 INTERNAL SECTION HAD CRACK INDICATION AT AREA 3 TOP OUTBOARD FASTENER USING SPOT AND RING PROBES.SDR IXXA20260612CC01Skin · corrodedRIGHT WING UPPER SKIN HAS CORROSION AT WBL 109.9 AND 70 INCHES FWD OF REAR SPAR.SDR IXXA20250622024Wire Harness · frayedPRIOR TO FLIGHT, GROUND LOADING REPORTED SMOKE FROM FORWARD LOWER CARGO FLOOR. CREW EVACUATED AIRCRAFT WITHOUT INCIDENT. AIRCRAFT GROUNDED FOR INSPECTIONS AND MAINTENANCE. FOLLOWING ADDITIONAL GENERAL VISUAL INSPECTIONS, FAULT ISOLATED TO FRAYED WIRE BUNDLE 7SDR IXXA2024091801Pin · corrodedRIGHT HAND OUTER PIVOT PIN DAMAGED AND CORRODED AMM 55-17-51SDR IXXA20240914001Skin · crackedLOWER TWO FASTENER HOLES IN SKIN AND BEARTRAP HAS CRACK INDICATION AT THE L1 DOOR CUTOUT AFT LOWER CORNER STA 335 JUST ABOVE STRINGER 20L.SDR IXXA20240913001Bracket · crackedNUMBER 2 ENGINE O/B CORE COWL NUMBER 2 LATCH HOUSING HAS CRACK ON LOWER FLANGESDR IXXA20240911001Panel · crackedRIGHT WING FIXED L/E COMPOSITE IS CRACKED ON UPPER SURFACE AFT OF TAI TELESCOPING DUCT CUTOUT.SDR IXXA2024091802Channel · crackedNUMBER 2 PYLON OUTBOARD SIDE INTERNAL SECTION JUST AFT AND BELOW HYDRAULIC RESERVIOR HAS CRACK CROSS BEAM. CRACKED LENGTH 1.5, FROM BS 955 TO 977, STRINGERS 24R TO 20RC.SDR IXXA2024091003Skin · damagedOUTER SKIN ON P32 DAMAGED EXPOSING HONEYCOMB EMANTING FROM THE FORWARD GROUND STUD LOCATIONSDR IXXA2024092003Electrical Box · damagedBONDING JUMPER STUD PULLED THROUGH P31 PANEL BOX BACK PANELSDR IXXA2024092002Support Bracket · crackedNUMBER 6 SLAT LOWER LEADING EDGE SUPPORT BRACKET, LOCATED AT THE CENTER AUX TRACK, IS CRACKEDSDR IXXA2024092001Support Bracket · crackedNO. 6 SLAT LOWER LEADING EDGE SUPPORT BRACKET, LOCATED AT THE BASE OF THE OUTBOARD AUX TRACK, IS CRACKEDSDR IXXA2024091002Bear Strap · crackedFWD FUSELAGE SKIN AND BEAR STRAP R1 DOOR CUTOUT HAS CRACK INDICATION LOWER FASTENER HOLE STA 335 JUST ABOVE STRINGER 20R. CRACKED LENGTH .5.SDR IXXA202407086048Trans Rectifier · faultedUPON POWER APPLICATION ON TAXI STRONG ELECTRICAL SMOKE AND FUMES, MULTIPLE DISCRETE LIGHTS HALF LIT, INDICATOR LIGHT 1 BREAKER POPPED. AIRCRAFT RETURNED TO BLOCKS. RANG OUT WIRING FROM LEFT GENERATOR CONTROL UNIT TO LEFT INTEGRATED DRIVE UNIT AND RANG OUT WIRISDR IXXA202301232007Battery · inoperativeFLASHLIGHT BEHIND FIRST OFICER HAD DEAD BATTERY AND NO FLASH INDICATION. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY BEHIND FIRT OFFICER'S SEAT IN ACCORDANCE WITH ATI LOPA DRAWING 25-767-01002 REVISION 3. OPERATIONAL CHECK GOOD.SDR IXXA2023012001Doubler · peelingDOUBLER PEELING ON TOP SURFACESDR IXXA2023011901Flap Track · corrodedIB FLAP TRACKS CORRODED..SDR IXXA2023011801Panel · delaminatedLW L/E 511PT DELAMSDR IXXA2023011501Structure · crackedNR 1 SLAT LWR TRAILING EDGE IS CRACKED, INBOARD END.SDR IXXA20221219150Flashlight · inoperativeDURING ROUTINE MAINTENANCE, FLIGHT DECK FLASHLIGHT IS INOPERTIVE. REMOVED AND REPLACED FLASH DECK FLASHLIGHT BATTERY IAW B767 AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR MK1Y02222021008Skin · dentedDURING MAINTENANCE INSPECTION FOUND A DENT WITH GOUGE ON FUSELAGE SKIN, SEC 41.SDR MK1Y02222021007Skin · damagedDURING MAINTENANCE INSPECTION FOUND MULTIPLE SCRATCHES (35) 3 CRACKS ON ENGINE NR 2 RT CORE COWL EXTERNAL SKIN.SDR MK1Y02222021006Skin · damagedDURING MAINTENANCE INSPECTION FOUND MULTIPLE SCRATCHES (25) ON ENGINE NR 1 LT CORE COWL EXTERNAL SKIN.SDR MK1Y02222021005Skin · corrodedDURING MAINTENANCE INSPECTION FOUND THREE (3) LOCATION OF CORROSION DAMAGE AT CENTER WING UPPER SKIN.SDR MK1Y02222021002Skin · damagedDURING MAINTENANCE INSPECTION FOUND SEVERAL BLEND OUTS OVER FLAT RIVET REPAIRS ON FUSELAGE SKIN.SDR MK1Y02222021001Skin · damagedDURING MAINTENANCE INSPECTION A DEFORMATION WHICH CONSIST OF SUNKEN AREA AND PROTRUDING AREA FOUND ON FUSELAGE SKIN AT STA 1263.
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